Any airplane with a pressure fueling system is going to have a volume based cutoff at the maximum allowed fuel volume for each tank (leaving the required expansion space). This feature is required by FAR/CS 25.979(b). On some airplanes it's float switch driven, and on others it's capacitive probe driven. Boeing uses the term volumetric top off, or VTO, for their feature in their literature. I don't know if Airbus uses the same name.